De-Icing of Aircraft Turbine Engine Inlets
-
1988-06-01
Details
-
Creators:
-
Corporate Creators:
-
Corporate Contributors:
-
Subject/TRT Terms:
-
Publication/ Report Number:
-
Resource Type:
-
Geographical Coverage:
-
Edition:Final Report
-
Contracting Officer:
-
Corporate Publisher:
-
Abstract:This document presents the results of an FAA investigation to determine the effects of using de-icing, as opposed to anti-icing, in aircraft turbine engine inlets. A literature search was conducted. Ice protection equipment technology was assessed. This report describes the icing/de-icing process, discusses de-ice system operation and performance and ice detector characteristics, and presents a method for determining the effects of the de-icing process on the turbine engine and its associated induction system.
-
Format:
-
Funding:
-
Collection(s):
-
Main Document Checksum:urn:sha-512:7d8a1662020fca9ffefc73bd98b1ea2092d6ba63c76c99f60bdb862c62dd7e51eee221b1a03694a8a1d8fce6f54bf15fa8953223aa6f87af1ee1cd905d6753e6
-
Download URL:
-
File Type: